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WO2009080013A1 - Procédé de production et de réparation d'un composant d'une turbine à gaz - Google Patents

Procédé de production et de réparation d'un composant d'une turbine à gaz Download PDF

Info

Publication number
WO2009080013A1
WO2009080013A1 PCT/DE2008/002133 DE2008002133W WO2009080013A1 WO 2009080013 A1 WO2009080013 A1 WO 2009080013A1 DE 2008002133 W DE2008002133 W DE 2008002133W WO 2009080013 A1 WO2009080013 A1 WO 2009080013A1
Authority
WO
WIPO (PCT)
Prior art keywords
component
blade
components
gas turbine
rotor
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/DE2008/002133
Other languages
German (de)
English (en)
Inventor
Erwin Bayer
Matija Burger
Martin Bussmann
Alexander Gindorf
Albin Platz
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MTU Aero Engines AG
Original Assignee
MTU Aero Engines GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by MTU Aero Engines GmbH filed Critical MTU Aero Engines GmbH
Priority to US12/808,738 priority Critical patent/US9333576B2/en
Priority to CA2708370A priority patent/CA2708370A1/fr
Priority to EP08864220A priority patent/EP2225065B1/fr
Priority to AT08864220T priority patent/ATE553872T1/de
Publication of WO2009080013A1 publication Critical patent/WO2009080013A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23H—WORKING OF METAL BY THE ACTION OF A HIGH CONCENTRATION OF ELECTRIC CURRENT ON A WORKPIECE USING AN ELECTRODE WHICH TAKES THE PLACE OF A TOOL; SUCH WORKING COMBINED WITH OTHER FORMS OF WORKING OF METAL
    • B23H3/00—Electrochemical machining, i.e. removing metal by passing current between an electrode and a workpiece in the presence of an electrolyte
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23H—WORKING OF METAL BY THE ACTION OF A HIGH CONCENTRATION OF ELECTRIC CURRENT ON A WORKPIECE USING AN ELECTRODE WHICH TAKES THE PLACE OF A TOOL; SUCH WORKING COMBINED WITH OTHER FORMS OF WORKING OF METAL
    • B23H9/00—Machining specially adapted for treating particular metal objects or for obtaining special effects or results on metal objects
    • B23H9/10—Working turbine blades or nozzles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/02—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating by means of a press ; Diffusion bonding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/02—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating by means of a press ; Diffusion bonding
    • B23K20/023—Thermo-compression bonding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/02—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating by means of a press ; Diffusion bonding
    • B23K20/028—Butt welding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/006—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine wheels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00—Restoring or reconditioning objects
    • B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
    • B23P6/005—Repairing turbine components, e.g. moving or stationary blades, rotors using only replacement pieces of a particular form
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/005—Repairing methods or devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3061—Fixing blades to rotors; Blade roots ; Blade spacers by welding, brazing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2230/00—Manufacture
    • F05B2230/20—Manufacture essentially without removing material
    • F05B2230/23—Manufacture essentially without removing material by permanently joining parts together
    • F05B2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
    • F05B2230/239—Inertia or friction welding
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/10—Manufacture by removing material
    • F05D2230/11—Manufacture by removing material by electrochemical methods
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49229—Prime mover or fluid pump making
    • Y10T29/49236—Fluid pump or compressor making
    • Y10T29/49238—Repairing, converting, servicing or salvaging

Definitions

  • the present invention relates to a method for producing and repairing a component consist of at least two metallic components joined together, in particular components of a gas turbine, wherein the joining and connecting of corresponding connecting surfaces of the components by means of a pressure welding process takes place and in the joining process an allowance in the region of a joining zone of the upset both connecting surfaces.
  • the invention further relates to a component produced by said method.
  • the inductor is energized at a constant frequency, which is generally above 0.75 MHz.
  • the frequency is also chosen depending on the geometry of the connection surfaces.
  • Further inductive Hochfrequenzpresssch spaverexcellenti are known from EP 1112141 Bl and EP 1140417 Bl.
  • a joining of components by means of linear friction welding is known.
  • this method is no longer reversible, since the existing distance geometry hinders the initiation of the frictional force.
  • the grooved component usually has an allowance, which still has to be processed to obtain a desired final contour.
  • An inventive method for producing and repairing a component consisting of at least two metallic components joined together, in particular components of a gas turbine comprises joining and connecting corresponding connection surfaces of the components by means of a pressure welding process.
  • a pressure welding process In this case, an allowance in the region of a joining zone of the two connecting surfaces is upset.
  • machining of the allowance is carried out by means of precise electrochemical removal (PECM) until a predefined final contour of the component is reached.
  • the pressure welding method is an inductive low-frequency or high-frequency compression welding method, the frequencies used being selected from a range between 0.05 and 2.5 MHz.
  • the precise electrochemical ablation takes place by means of a synchronous, on all sides of the component simultaneously abtragenden lowering process.
  • the removal can be carried out by means of a hollow electrode. But it is also possible that the removal is carried out by means of at least one each guided on opposite sides of the component electrodes. Due to the synchronous lowering process, a possible damage supply, in particular a possible bending of the machined areas of the component reliably prevented.
  • electrically conductive guide elements can be arranged on the electrodes and / or the component for carrying the electrolyte. These can also have elastic properties if required. Due to the targeted electrolyte guidance advantageously no impermissible etching attack takes place on already having a final contour areas of the component to be machined.
  • a passivation of the non-machinable regions of the component is carried out during precise electrochemical removal. This can be done, for example, by setting a suitable electrochemical potential difference between the component and the electrode. However, it is also possible that the passivation takes place by applying electrically insulating materials to the component surface. Also by the passivation of the non-machined areas of the component, in particular the already having the final contour areas of the component they are protected against an undesired etching attack. In this case, the passivation of the already having in the final contour areas of the component with the targeted Elektrolytbowung, as described above, be combined.
  • the contour of each electrode is adapted to the final contour of the component. This makes it possible that the processing step of both sides and simultaneous lowering can be performed very quickly and precisely.
  • the electrodes perform oscillating movements during lowering.
  • the electrode gap can be completely rinsed with fresh, unused electrolyte. Possible gas bubbles and electrode sludge are reliably removed from the electrode gap.
  • a current pulse is emitted only in the region of the smallest distance between the electrode and the component to be processed. In the area of the maximum distance between the electrode and the workpiece to be machined, the electrolyte rinse then takes place.
  • the first component is a blade or a part of a blade of a rotor in a gas turbine and the second component is a ring or a disk of the rotor or a blade root arranged on the circumference of the ring or the disk.
  • This relates in particular to rotor blades (BLISK or BLING) produced integrally with a rotor disk or a supporting ring.
  • the components are parts of a blade of a rotor in a gas turbine.
  • the method according to the invention enables material-saving production and repair of blisks and blings, in particular with medium and small blades.
  • material combinations ie the use of different metallic materials for blade and disc or blade and ring are possible.
  • an oversize area is generated, which leads to a leveling of the outer contour, even in the case of repair of the corresponding component.
  • targeted electrolyte guidance and / or passivation of the final contour areas of the blisk or Bling these areas are also protected by an impermissible material removal or etching attack.
  • it is prevented that large unilateral bending forces act on the blade, since, for example, a two-sided synchronous and low-force removal takes place via the precise electrochemical removal process.
  • a component of a gas turbine according to the invention consists of at least a first and a second component and is produced by a method according to the invention described above.
  • the first component may be a blade or a part of a blade of a rotor in a gas turbine and the second component may be a ring or a disk of the rotor or a blade root arranged on the circumference of the ring or the disk.
  • This particularly relates to rotor blades (BLISK or BLING) made integrally with a rotor disk or a supporting ring.
  • the components are parts of a blade of a rotor in a gas turbine.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Abstract

L'invention concerne un procédé de production et de réparation d'un composant comprenant au moins deux éléments métalliques assemblés entre eux, en particulier des éléments d'une turbine à gaz, l'assemblage et la liaison des surfaces correspondantes desdits éléments s'effectuant par soudage par pression. Une surépaisseur est refoulée dans la région d'une zone d'assemblage des deux surfaces à lier et, après assemblage des deux éléments, on procède à un usinage de la surépaisseur par érosion électrochimique précise (PECM), jusqu'à obtention d'un profil définitif prédéfini du composant. L'invention concerne en outre un composant d'une turbine à gaz fabriqué conformément au procédé de l'invention.
PCT/DE2008/002133 2007-12-22 2008-12-18 Procédé de production et de réparation d'un composant d'une turbine à gaz Ceased WO2009080013A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US12/808,738 US9333576B2 (en) 2007-12-22 2008-12-18 Method for producing and repairing a part, and part of a gas turbine
CA2708370A CA2708370A1 (fr) 2007-12-22 2008-12-18 Procede de production et de reparation d'un composant d'une turbine a gaz
EP08864220A EP2225065B1 (fr) 2007-12-22 2008-12-18 Procédé de production et de réparation d'un composant
AT08864220T ATE553872T1 (de) 2007-12-22 2008-12-18 Verfahren zur herstellung und reparatur eines bauteils

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007062559.8 2007-12-22
DE102007062559A DE102007062559A1 (de) 2007-12-22 2007-12-22 Verfahren zur Herstellung und Reparatur eines Bauteils und Bauteil einer Gasturbine

Publications (1)

Publication Number Publication Date
WO2009080013A1 true WO2009080013A1 (fr) 2009-07-02

Family

ID=40673214

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/DE2008/002133 Ceased WO2009080013A1 (fr) 2007-12-22 2008-12-18 Procédé de production et de réparation d'un composant d'une turbine à gaz

Country Status (6)

Country Link
US (1) US9333576B2 (fr)
EP (1) EP2225065B1 (fr)
AT (1) ATE553872T1 (fr)
CA (1) CA2708370A1 (fr)
DE (1) DE102007062559A1 (fr)
WO (1) WO2009080013A1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009043184A1 (de) * 2009-09-26 2011-04-07 Mtu Aero Engines Gmbh Verfahren zur Reparatur eines integralen Rotors und integraler Rotor
DE102010012779B3 (de) * 2010-03-25 2011-09-29 Mtu Aero Engines Gmbh Verfahren zum Herstellen und/oder Reparieren eines integral beschaufelten Rotors
JP6583439B2 (ja) * 2016-02-01 2019-10-02 株式会社Ihi 線形摩擦接合装置、並びに、治具の位置調整装置及び位置調整方法
CN116728009A (zh) * 2023-06-13 2023-09-12 西安理工大学 基于电脉冲调控钛合金摩擦焊接头组织的方法

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Also Published As

Publication number Publication date
ATE553872T1 (de) 2012-05-15
DE102007062559A1 (de) 2009-06-25
US20110002789A1 (en) 2011-01-06
EP2225065B1 (fr) 2012-04-18
US9333576B2 (en) 2016-05-10
CA2708370A1 (fr) 2009-07-02
EP2225065A1 (fr) 2010-09-08

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